Search filter

    • Year
      1906
      2018
    • Length
      13 m
      20 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      25 m2
      39 m2
    • Wingspan (Beam)
      13 m
      21 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      1
      26
    • Disc area
      1 m2
      460 m2
    • Main rotor diameter
      1 m
      62 m
    • Rotor number
      1 qt
      8 qt
    • Blades per rotor
      4 qt
      5 qt
    • Disc loading
      17 kg/m2
      73 kg/m2
    • Tail rotor diameter
      0 m
      5 m
    • Empty weight
      2991 kg
      4487 kg
    • Max. takeoff weight (Gross weight)
      5120 kg
      7680 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      1872 kg
      2808 kg
    • Payload
      1872 kg
      2808 kg
    • Capacity passengers
      15 per.
      23 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      5506 km/h
      8260 km/h
    • Сruise Speed
      281 km/h
      423 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      107 km/h
      1050 km/h
    • Fuel Capacity
      23 l
      320000 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      1240 hp
      1860 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6828 m
      10242 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      888 km
      1334 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      360 m/min
      540 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      18 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      219 qt
      329 qt
    • Price
      5600000 USD
      8400000 USD

Dornier Do 228

TypeAircraft
Company

Dornier Flugzeugwerke

Fairchild Aircraft

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
16.6
88.7
Height (m)
0.6
 
4.9
50.1
Wings
Wing area (m2)
1.1
 
32
925
Wingspan (Beam) (m)
0.1
 
17.0
95
Weights
Empty weight (kg)
8
 
3,739
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,400
575,000
Capacity
Crew (per.)
1
 
2
112
Useful load (kg)
26.4
 
2,340
90,700
Payload (kg)
23
 
2,340
122,470
Capacity passengers (per.)
1
 
19
400
Speeds
Max. Speed (km/h)
25
 
6,883
28,165
Сruise Speed (km/h)
52
 
351.9
3,087
at appox 15 degree C with 85% torque
Power
Total Power (hp)
0.4
 
1,550
60,000
2 powerplants 775 hp each
Performance
Service ceiling (m)
0.6
 
8,535
161,544
Range (Ferry range) (km)
4
 
1,111
40,700
with full payload
Dynamic Performance
Rate of climb (m/min)
1.9
 
450
36,000
Stat
Number built (qt)
0
 
274
43,000
Price (USD)
41.5
 
7.0 million
750.0 million
Introduction 1981
First flight 21.03.1981

Similar aircraft

Get more

Museums on map

Museums

Comments